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A Novel Cooperative Control System of Multi-Missile Formation under Uncontrollable Speed
2021
IEEE Access
This article investigates a novel cooperative control system based on the sliding mode variable structure control theory for multi-missile formation flight. It is desired in practice to form and maintain the formation under the premise of uncontrollable missile speed. First, under the inertial coordinate system, we obtain the model of the formation control problem using the relative position of the leader to the follower. Then, we perform acceleration conversion and combine it to this model,
doi:10.1109/access.2021.3049571
fatcat:rkhc6snxgjdprish6fdotbbaxm